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首页> 外文期刊>Journal of Aeronautics, Astronautics and Aviation, A >UAV 2-D Track Smoothing Method Base on Non-uniform B-spline Interpolation
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UAV 2-D Track Smoothing Method Base on Non-uniform B-spline Interpolation

机译:基于非均匀B样条插值的无人机二维航迹平滑方法

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摘要

The initial UAV tracks produced by intelligent optimization algorithm cannot meet the requirements of UAV flight performance. So smoothing the UAV tracks is necessary. This paper adopts a method of non-uniform B-spline curve interpolation to solve this problem. Firstly, the paper analyses and discusses the research methods of track smoothing carried on recently. Then considering B-spline basis function and B-spline curve properties and making use of the problem of uneven parameters distribution for the flight track-smoothing, this paper proposes the flow-chart of non-uniform B-spline interpolation method and then simulated by Matlab language to verify the performance of the proved algorithm. The simulation results show that the smoothing track has many advantages, such as natural transition, no heading mutation, and not through the danger zone. This method achieves to preserve the convexity of the curve and passes all the track nodes, which make the smoothing track approximate with the original one. In addition, the fuel costs and the threat costs do not change dramatically. This method meets the flight performance requirements of UAV.
机译:智能优化算法产生的初始无人机航迹不能满足无人机飞行性能要求。因此,平滑无人机航迹是必要的。本文采用非均匀B样条曲线插值的方法来解决该问题。首先,本文对最近进行的轨道平滑研究方法进行了分析和讨论。在考虑B样条基函数和B样条曲线特性的基础上,利用参数分布不均匀的问题解决了航迹平滑问题,提出了非均匀B样条插值方法的流程图,并通过用Matlab语言验证了该算法的性能。仿真结果表明,该平滑轨道具有许多优点,如自然过渡,无航向突变和不穿越危险区域。该方法可以保留曲线的凸度并通过所有轨道节点,从而使平滑轨道与原始轨道近似。此外,燃料成本和威胁成本不会发生太大变化。该方法满足了无人机的飞行性能要求。

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